Processes and systems for depositing coating systems, and components coated therewith
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[0019]The present invention is generally applicable to components that may be coated by a spraying process wherein the design of the components provides a line-of-site access angle to the surface to be coated of less than 30 degrees. Notable examples of such components include gas turbine engine components, such as the gas turbine component 10 of FIG. 1 comprising seal teeth 12. Although the invention will be described hereinafter in reference to the gas turbine component 10, it will be appreciated that this is exemplary and that the invention has application to other components. Coatings formed by the invention may be comprised of any suitable material such as, but not limited to, ceramics, metallics, cermets, and carbides.
[0020]FIGS. 3 and 4 represent a component 10 of the type shown in FIG. 1 undergoing a thermal spray process in accordance with an embodiment of the present invention. As such, FIGS. 3 and 4 represent a seal tooth 12 of the component 10 as being thermal sprayed wi...
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